AU2015240681B2 - High strength Ni-Cr-Mo-W-Nb-Ti welding product and method of welding and weld deposit using the same - Google Patents
High strength Ni-Cr-Mo-W-Nb-Ti welding product and method of welding and weld deposit using the same Download PDFInfo
- Publication number
- AU2015240681B2 AU2015240681B2 AU2015240681A AU2015240681A AU2015240681B2 AU 2015240681 B2 AU2015240681 B2 AU 2015240681B2 AU 2015240681 A AU2015240681 A AU 2015240681A AU 2015240681 A AU2015240681 A AU 2015240681A AU 2015240681 B2 AU2015240681 B2 AU 2015240681B2
- Authority
- AU
- Australia
- Prior art keywords
- weld deposit
- filler metal
- welding filler
- niobium
- less
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Active
Links
- 238000003466 welding Methods 0.000 title claims abstract description 109
- 238000000034 method Methods 0.000 title claims abstract description 22
- 229910020012 Nb—Ti Inorganic materials 0.000 title description 3
- 229910052751 metal Inorganic materials 0.000 claims abstract description 103
- 239000002184 metal Substances 0.000 claims abstract description 103
- 239000000945 filler Substances 0.000 claims abstract description 85
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 claims abstract description 84
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 claims abstract description 76
- 239000010955 niobium Substances 0.000 claims abstract description 47
- 229910052742 iron Inorganic materials 0.000 claims abstract description 42
- 229910052758 niobium Inorganic materials 0.000 claims abstract description 42
- 229910052759 nickel Inorganic materials 0.000 claims abstract description 37
- GUCVJGMIXFAOAE-UHFFFAOYSA-N niobium atom Chemical compound [Nb] GUCVJGMIXFAOAE-UHFFFAOYSA-N 0.000 claims abstract description 37
- 229910052715 tantalum Inorganic materials 0.000 claims abstract description 31
- 239000010936 titanium Substances 0.000 claims abstract description 31
- 239000011651 chromium Substances 0.000 claims abstract description 30
- 229910052750 molybdenum Inorganic materials 0.000 claims abstract description 30
- GUVRBAGPIYLISA-UHFFFAOYSA-N tantalum atom Chemical compound [Ta] GUVRBAGPIYLISA-UHFFFAOYSA-N 0.000 claims abstract description 30
- 229910052721 tungsten Inorganic materials 0.000 claims abstract description 29
- 229910052804 chromium Inorganic materials 0.000 claims abstract description 28
- 229910052719 titanium Inorganic materials 0.000 claims abstract description 28
- 239000010937 tungsten Substances 0.000 claims abstract description 28
- 239000011733 molybdenum Substances 0.000 claims abstract description 27
- WFKWXMTUELFFGS-UHFFFAOYSA-N tungsten Chemical compound [W] WFKWXMTUELFFGS-UHFFFAOYSA-N 0.000 claims abstract description 27
- ZOKXTWBITQBERF-UHFFFAOYSA-N Molybdenum Chemical compound [Mo] ZOKXTWBITQBERF-UHFFFAOYSA-N 0.000 claims abstract description 26
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 claims abstract description 26
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 claims abstract description 24
- 229910052782 aluminium Inorganic materials 0.000 claims abstract description 24
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 claims abstract description 23
- 229910052799 carbon Inorganic materials 0.000 claims abstract description 22
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 claims abstract description 21
- 239000010941 cobalt Substances 0.000 claims abstract description 17
- 229910017052 cobalt Inorganic materials 0.000 claims abstract description 17
- GUTLYIVDDKVIGB-UHFFFAOYSA-N cobalt atom Chemical compound [Co] GUTLYIVDDKVIGB-UHFFFAOYSA-N 0.000 claims abstract description 16
- 229910000831 Steel Inorganic materials 0.000 claims description 16
- 239000012895 dilution Substances 0.000 claims description 16
- 238000010790 dilution Methods 0.000 claims description 16
- 239000010959 steel Substances 0.000 claims description 16
- 239000002245 particle Substances 0.000 claims description 14
- 238000002844 melting Methods 0.000 claims description 8
- 230000008018 melting Effects 0.000 claims description 8
- 238000001816 cooling Methods 0.000 claims description 6
- 229910000990 Ni alloy Inorganic materials 0.000 claims description 5
- 229910045601 alloy Inorganic materials 0.000 description 23
- 239000000956 alloy Substances 0.000 description 23
- 150000002739 metals Chemical class 0.000 description 17
- 239000000463 material Substances 0.000 description 14
- 229910001026 inconel Inorganic materials 0.000 description 13
- 239000000203 mixture Substances 0.000 description 12
- 230000000694 effects Effects 0.000 description 10
- 238000005728 strengthening Methods 0.000 description 10
- 230000009286 beneficial effect Effects 0.000 description 9
- 238000005260 corrosion Methods 0.000 description 9
- 230000007797 corrosion Effects 0.000 description 9
- 238000012360 testing method Methods 0.000 description 9
- 238000009864 tensile test Methods 0.000 description 8
- 239000011572 manganese Substances 0.000 description 6
- 239000011159 matrix material Substances 0.000 description 6
- 239000010953 base metal Substances 0.000 description 5
- 230000015572 biosynthetic process Effects 0.000 description 5
- 239000011324 bead Substances 0.000 description 4
- 239000011575 calcium Substances 0.000 description 4
- 238000005336 cracking Methods 0.000 description 4
- 230000001627 detrimental effect Effects 0.000 description 4
- 239000011777 magnesium Substances 0.000 description 4
- 238000007711 solidification Methods 0.000 description 4
- 230000008023 solidification Effects 0.000 description 4
- OYPRJOBELJOOCE-UHFFFAOYSA-N Calcium Chemical compound [Ca] OYPRJOBELJOOCE-UHFFFAOYSA-N 0.000 description 3
- FYYHWMGAXLPEAU-UHFFFAOYSA-N Magnesium Chemical compound [Mg] FYYHWMGAXLPEAU-UHFFFAOYSA-N 0.000 description 3
- 229910052791 calcium Inorganic materials 0.000 description 3
- 230000004927 fusion Effects 0.000 description 3
- BHEPBYXIRTUNPN-UHFFFAOYSA-N hydridophosphorus(.) (triplet) Chemical compound [PH] BHEPBYXIRTUNPN-UHFFFAOYSA-N 0.000 description 3
- 229910052749 magnesium Inorganic materials 0.000 description 3
- 238000004519 manufacturing process Methods 0.000 description 3
- 239000003208 petroleum Substances 0.000 description 3
- 238000004881 precipitation hardening Methods 0.000 description 3
- 229910052710 silicon Inorganic materials 0.000 description 3
- 239000010703 silicon Substances 0.000 description 3
- 239000011593 sulfur Substances 0.000 description 3
- 229910052717 sulfur Inorganic materials 0.000 description 3
- XUIMIQQOPSSXEZ-UHFFFAOYSA-N Silicon Chemical compound [Si] XUIMIQQOPSSXEZ-UHFFFAOYSA-N 0.000 description 2
- NINIDFKCEFEMDL-UHFFFAOYSA-N Sulfur Chemical compound [S] NINIDFKCEFEMDL-UHFFFAOYSA-N 0.000 description 2
- 239000008186 active pharmaceutical agent Substances 0.000 description 2
- 238000007792 addition Methods 0.000 description 2
- 238000005253 cladding Methods 0.000 description 2
- 238000010438 heat treatment Methods 0.000 description 2
- 238000005304 joining Methods 0.000 description 2
- 229910052748 manganese Inorganic materials 0.000 description 2
- 239000003921 oil Substances 0.000 description 2
- 238000001556 precipitation Methods 0.000 description 2
- 238000001878 scanning electron micrograph Methods 0.000 description 2
- 230000035945 sensitivity Effects 0.000 description 2
- 239000006104 solid solution Substances 0.000 description 2
- PWHULOQIROXLJO-UHFFFAOYSA-N Manganese Chemical compound [Mn] PWHULOQIROXLJO-UHFFFAOYSA-N 0.000 description 1
- 238000000137 annealing Methods 0.000 description 1
- 238000005266 casting Methods 0.000 description 1
- 230000003749 cleanliness Effects 0.000 description 1
- 239000011248 coating agent Substances 0.000 description 1
- 238000000576 coating method Methods 0.000 description 1
- 230000007423 decrease Effects 0.000 description 1
- 230000003247 decreasing effect Effects 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 239000006185 dispersion Substances 0.000 description 1
- 238000006073 displacement reaction Methods 0.000 description 1
- 230000007717 exclusion Effects 0.000 description 1
- 230000004907 flux Effects 0.000 description 1
- 239000012535 impurity Substances 0.000 description 1
- 238000007689 inspection Methods 0.000 description 1
- 239000000155 melt Substances 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 230000035515 penetration Effects 0.000 description 1
- 238000002360 preparation method Methods 0.000 description 1
- 230000001737 promoting effect Effects 0.000 description 1
- 238000012797 qualification Methods 0.000 description 1
- SYUHGPGVQRZVTB-UHFFFAOYSA-N radon atom Chemical compound [Rn] SYUHGPGVQRZVTB-UHFFFAOYSA-N 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
- 239000000126 substance Substances 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
- B23K35/00—Rods, electrodes, materials, or media, for use in soldering, welding, or cutting
- B23K35/22—Rods, electrodes, materials, or media, for use in soldering, welding, or cutting characterised by the composition or nature of the material
- B23K35/24—Selection of soldering or welding materials proper
- B23K35/30—Selection of soldering or welding materials proper with the principal constituent melting at less than 1550 degrees C
- B23K35/3033—Ni as the principal constituent
- B23K35/304—Ni as the principal constituent with Cr as the next major constituent
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
- B23K35/00—Rods, electrodes, materials, or media, for use in soldering, welding, or cutting
- B23K35/02—Rods, electrodes, materials, or media, for use in soldering, welding, or cutting characterised by mechanical features, e.g. shape
- B23K35/0255—Rods, electrodes, materials, or media, for use in soldering, welding, or cutting characterised by mechanical features, e.g. shape for use in welding
- B23K35/0261—Rods, electrodes, wires
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
- B23K35/00—Rods, electrodes, materials, or media, for use in soldering, welding, or cutting
- B23K35/02—Rods, electrodes, materials, or media, for use in soldering, welding, or cutting characterised by mechanical features, e.g. shape
- B23K35/0255—Rods, electrodes, materials, or media, for use in soldering, welding, or cutting characterised by mechanical features, e.g. shape for use in welding
- B23K35/0261—Rods, electrodes, wires
- B23K35/0266—Rods, electrodes, wires flux-cored
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
- B23K35/00—Rods, electrodes, materials, or media, for use in soldering, welding, or cutting
- B23K35/22—Rods, electrodes, materials, or media, for use in soldering, welding, or cutting characterised by the composition or nature of the material
- B23K35/24—Selection of soldering or welding materials proper
- B23K35/30—Selection of soldering or welding materials proper with the principal constituent melting at less than 1550 degrees C
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
- B23K35/00—Rods, electrodes, materials, or media, for use in soldering, welding, or cutting
- B23K35/22—Rods, electrodes, materials, or media, for use in soldering, welding, or cutting characterised by the composition or nature of the material
- B23K35/36—Selection of non-metallic compositions, e.g. coatings, fluxes; Selection of soldering or welding materials, conjoint with selection of non-metallic compositions, both selections being of interest
- B23K35/368—Selection of non-metallic compositions of core materials either alone or conjoint with selection of soldering or welding materials
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
- B23K9/00—Arc welding or cutting
- B23K9/16—Arc welding or cutting making use of shielding gas
- B23K9/164—Arc welding or cutting making use of shielding gas making use of a moving fluid
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C19/00—Alloys based on nickel or cobalt
- C22C19/03—Alloys based on nickel or cobalt based on nickel
- C22C19/05—Alloys based on nickel or cobalt based on nickel with chromium
- C22C19/051—Alloys based on nickel or cobalt based on nickel with chromium and Mo or W
- C22C19/055—Alloys based on nickel or cobalt based on nickel with chromium and Mo or W with the maximum Cr content being at least 20% but less than 30%
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C19/00—Alloys based on nickel or cobalt
- C22C19/03—Alloys based on nickel or cobalt based on nickel
- C22C19/05—Alloys based on nickel or cobalt based on nickel with chromium
- C22C19/051—Alloys based on nickel or cobalt based on nickel with chromium and Mo or W
- C22C19/056—Alloys based on nickel or cobalt based on nickel with chromium and Mo or W with the maximum Cr content being at least 10% but less than 20%
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Materials Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Physics & Mathematics (AREA)
- Plasma & Fusion (AREA)
- Arc Welding In General (AREA)
Abstract
A welding filler metal or a welding filler metal product having, in weight percent: 17.0-23.0% chromium, 5.0-12.0% molybdenum, 3.0-11.0% tungsten, 3.0-5.0% niobium, 0-2.0% tantalum, 1.2-3.0% titanium, 0.005-1.50% aluminum, 0.0005-0.100% carbon, <2.0% iron, <5.0% cobalt, and balance nickel wherein the nickel is 56.0-65.0%. A weld deposit formed from the welding filler metal has a minimum yield strength in the as-welded condition of at least 72 ksi (496 MPa). Also, a weld deposit and a method of forming a weld deposit comprising, in weight percent: 17.0-23.0% chromium, 5.0-12.0% molybdenum, 3.0-11.0% tungsten, 3.0-5.0% niobium, 0-2.0% tantalum, 1.2-3.0% titanium, 0.005-1.50% aluminum, 0.0005-0.100% carbon, <8.0% iron, <5.0% cobalt, and balance nickel wherein the nickel is 56.0-65.0%. The weld deposit has a minimum yield strength in the as-welded condition of at least 72 ksi (496 MPa).
Description
HIGH STRENGTH NI-CR-MQ-W-NB-TI WELDING PRODUCT AND METHOD OF
WELDING AND WELD DEPOSIT USING THE SAME
CROSS REFERENCE TO RELATED APPLICATIONS [0001] This application claims priority to United States Provisional Application Serial No. 61/975,358 filed on April 4, 2014 and United States Provisional Application Serial No. 61/989,188 filed on May 6, 2014, both of which are incorporated by reference in their entireties.
BACKGROUND OF THE INVENTION
Field of the Invention [0002] The present invention relates to a high strength Ni-Cr-Mo-W-Nb-Ti welding filler metal and weld deposit and a method of creating a weld deposit using the welding filler metal and, more particularly, to a Ni-Cr-Mo-W-Nb-Ti welding filler metal used to produce a weld deposit having high yield strength in the as-welded condition.
Description of Related Art [0003] During off-shore exploration, development, and production of crude petroleum, there is a need for laying pipe at a rapid rate in order to minimize the time of employment of very expensive “lay barges”. This need is met by the concept of “Reeling” long lengths of ID clad pipe welded end-to-end on dry land at facilities called “Spool Bases”. These facilities are quite expensive to operate and have multiple stations within the base for preparation, welding, serially sequenced NDE inspection, and coating of long lengths of high-strength IDclad X-65, X-70, and X-80 pipe. While at sea, joining ends of reels is even more timesensitive than that required at Spool Bases due to the elevated cost of lay-barge operations. Spool Base operators and lay-barge welders are reluctant to use precipitation-hardened weld metals such as INCO-WELD Filler Metal 725NDUR that require elevated temperature hold times to develop high strength via precipitation hardening because it would slow the process and perhaps have a negative effect on the high strength steel pipes.
[0004] Due to the desire to operate these “Spool Bases” most efficiently, gas metal arc welding (GMAW) is used because of the faster rate of welding.
- 1 2015240681 17 Oct 2017 [0005] Thus, there is a need for a welding wire that may be used with the gas metal arc welding process that exhibits the same or slightly better corrosion resistance in sour oil and gas applications than the INCONEL® alloy 625 (58.0% min. Ni, 20.0-23.0% Cr, 5.0% max. Fe, 8.0-10.0% Mo, 3.15-4.15% Nb, 0.10% max. C, 0.50% max. Mn, 0.50% max. Si, 0.015% max. P, 0.015% max. S, 0.40% max. Al, 0.40% max. Ti, and 1.0% max. Co, in weight %). This wire is needed to weld ID-clad high-strength pipes made of American Petroleum Industry Specification 5L (API 5L) X-65, X-70, and X-80 steels while providing greater yield strengths in the as-welded condition than each of the base steels being welded. The desirable weld metal would have a yield strength that is approximately 14.5 ksi (100 MPa) greater than the minimum yield strength specified for the pipe that is being welded since qualifications require that transverse two-thickness (2T) 180 degree bends must be performed on the actual pipe being used, and transverse tensile tests must fail in the base metal. Additionally, an overmatch in strength would be desirable to facilitate “Reeling” without the possibility of kinking at or near the welds.
[0006] Throughout this specification the word comprise, or variations such as comprises or comprising, will be understood to imply the inclusion of a stated element, integer or step, or group of elements, integers or steps, but not the exclusion of any other element, integer or step, or group of elements, integers or steps.
[0007] Any discussion of documents, acts, materials, devices, articles or the like which has been included in the present specification is not to be taken as an admission that any or all of these matters form part of the prior art base or were common general knowledge in the field relevant to the present disclosure as it existed before the priority date of each of the appended claims.
SUMMARY OF THE INVENTION [0008] A welding filler metal comprising in weight percent: 17.0 to 23.0% chromium, 5.0 to 12.0% molybdenum, 3.0 to 11.0% tungsten, 3.0 to 5.0% niobium, 0 to 2.0% tantalum, 1.2 to 3.0% titanium, 0.005 to 1.50% aluminum, 0.0005 to 0.100% carbon, less than 2.0% iron, less than 5.0% cobalt, and balance nickel wherein the nickel is 56.0 to 65.0%. A weld deposit formed from the welding filler metal has a minimum yield strength in an as-welded condition of at least 72 ksi (496 MPa). The welding filler metal may comprise 64.0% maximum nickel, 22.0% maximum chromium, 10.5% maximum molybdenum, 9.5% maximum tungsten, 4.5% maximum niobium, 1.5% maximum tantalum, 2.5% maximum titanium, 1.25% maximum aluminum, 0.075% maximum carbon, 1.0% maximum iron, and
-22015240681 17 Oct 2017
4.0% maximum cobalt. The welding filler metal may comprise 57.0% minimum nickel, 18.0% minimum chromium, 5.5% minimum molybdenum, 3.5% minimum tungsten, 3.3% minimum niobium, 1.3% minimum titanium, 0.10% minimum aluminum, and 0.005% minimum carbon. The welding filler metal may comprise 62.0% maximum nickel, 21.0% maximum chromium, 9.0% maximum molybdenum, 8.0% maximum tungsten, 4.0% maximum niobium, 1.0% maximum tantalum, 2.0% maximum titanium, 1.00% maximum aluminum, 0.050% maximum carbon, 0.5% maximum iron, and 2.5% maximum cobalt. The welding filler metal may comprise 58.0% minimum nickel, 19.0% minimum chromium, 6.0% minimum molybdenum, 4.0% minimum tungsten, 3.5% minimum niobium, 1.4% minimum titanium, 0.15% minimum aluminum, and 0.010% minimum carbon. The welding filler metal may comprise a minimum of 3.5% niobium + tantalum. The welding filler metal may comprise a maximum of 6.0% niobium + tantalum.
[0009] A welding filler metal product having the composition described above for the welding filler metal. A weld deposit formed from the welding filler metal product has a minimum yield strength in an as-welded condition of at least 72 ksi (496 MPa). The welding filler metal product may be in the form of a tubular wire or a flux-cored wire.
[0010] A weld deposit comprising, in weight percent: 17.0 to 23.0% chromium, 5.0 to 12.0% molybdenum, 3.0 to 11.0% tungsten, 3.0 to 5.0% niobium, 0 to 2.0% tantalum, 1.2 to 3.0% titanium, 0.005 to 1.50% aluminum, 0.0005 to 0.100% carbon, less than 8.0% iron, less than 5.0% cobalt, and balance nickel wherein the nickel is 56.0 to 65.0%. The weld deposit has a minimum yield strength in an as-welded condition of at least 72 ksi (496 MPa). The weld deposit may comprise 64.0% maximum nickel, 22.0% maximum chromium, 10.5% maximum molybdenum, 9.5% maximum tungsten, 4.5% maximum niobium, 1.5% maximum tantalum, 2.5% maximum titanium, 1.25% maximum aluminum, 0.075% maximum carbon, 7.0% maximum iron, and 4.0% maximum cobalt. The weld deposit may comprise 57.0% minimum nickel, 18.0% minimum chromium, 5.5% minimum molybdenum, 3.5% minimum tungsten, 3.3% minimum niobium, 1.3% minimum titanium, 0.10% minimum aluminum, and 0.005% minimum carbon. The weld deposit may comprise 62.0% maximum nickel, 21.0% maximum chromium, 9.0% maximum molybdenum, 8.0% maximum tungsten, 4.0% maximum niobium, 1.0% maximum tantalum, 2,0% maximum titanium, 1.00% maximum aluminum, 0.050% maximum carbon, 5.0% maximum iron, and 2.5% maximum cobalt. The weld deposit may comprise 58.0% minimum nickel, 19.0% minimum chromium, 6.0% minimum molybdenum, 4.0% minimum tungsten, 3.5% minimum niobium, 1.4% minimum titanium,0.15% minimum aluminum, and 0.010% carbon. The weld deposit may comprise a -3 2015240681 17 Oct 2017 minimum of 3.5% niobium + tantalum. The weld deposit may comprise a maximum of 6.0% niobium + tantalum.
[0011] The weld deposit may have a microstructure including finely dispersed second phase particles. The second phase particles may be less than 5 pm. Elongation of the weld deposit may be at least 20%. Toughness of the weld deposit may be at least 50 J at -50°F. [0012] A method of producing a weld deposit comprising providing a welding tiller metal or welding filler metal product as described above, melting and cooling the welding tiller metal or welding filler metal product to create a weld deposit; and limiting iron dilution of the weld deposit during melting and cooling such that an as-welded weld deposit contains less than 8% iron, wherein the weld deposit has a minimum yield strength in the as-welded condition of at least 72 ksi (496 MPa). The melting and cooling of the welding tiller metal or welding filler metal product may be accomplished by gas metal arc welding (GMAW) or gas tungsten arc welding (GTAW). The welding filler metal or welding filler metal product may be melted and cooled in a narrow groove joint between two steel components wherein the namow groove joint has an included angle of 2-5 degrees. The steel components may be clad on at least one side with a nickel alloy.
[0013] A weldment comprising at least two high-strength steel components, each of the components individually having a minimum yield strength of 65 ksi (448 MPa) connected by a weld deposit having the composition described above and having a minimum yield strength in an as-welded condition of at least 72 ksi (496 MPa).
BRIEF DESCRIPTION OF THE DRAWING(S) [0014] FIG. 1 is a scanning electron micrograph of the microstructure of one embodiment of the inventive weld deposit showing small second phase particles;
[0015] FIG. 2 is a photograph of samples of X-65 pipe welded with the inventive welding filler metal HV1654 after tensile testing; and [0016] FIG. 3 is a photograph of samples of X-65 pipe welded with the inventive welding filler metal ΗVI708 after tensile testing
DESCRIPTION OF THE INVENTION [0017] All yield strengths cited herein were measured at a 0.2% offset and ail compositions are given in weight percent.
[0018] The present invention is directed to a welding filler metal and weld deposit and a method of using the welding filler metal to achieve a weld deposit that exhibits good
-42015240681 17 Oct 2017 corrosion resistance, preferably the same or slightly better than INCONEL® alloy 625 (58.0% min. Ni, 20.0-23.0% Cr, 5.0% max. Fe, 8.0-10.0% Mo, 3.15-4.15% Nb, 0.10% max. C, 0.50% max. Mn, 0.50% max. Si, 0.015% max. P, 0.015% max. S, 0.40% max. Al, 0.40% max. Ti, and 1.0% max. Co) in sour oil and gas applications yet provides greater yield strengths in the as-welded condition than each of the base steels being welded, American Petroleum Industry Specification 5L (API 5L) X-65, X-70, and X-80 steels. The weld deposit preferably has an as-welded yield strength that is at least 14.5 ksi (100 MPa) greater than the minimum yield strength specified for the pipe that is being welded.
[0019] For X-65 pipe having a required minimum yield strength of 65 ksi (448 MPa), the typical yield strength is around 72-74 ksi (496-510 MPa) and the highest expected yield strength is around 75-77 ksi (517-531 MPa). Likewise, for X-70 pipe having a required minimum yield strength of 70 ksi (483 MPa), the typical yield strength is 75-77 ksi (517-531 MPa) while the highest expected yield strength is around 80-82 ksi (552-565 MPa), and for X-80 pipe having a required minimum yield strength of 80 ksi (552 MPa), the typical yield strength is around 84-86 ksi (579-593 MPa) with the maximum expected yield strength of about 88-90 ksi (607-621 MPa). Thus, in order to have a weld deposit with a yield strength at least 14.5 ksi (100 MPa) greater than the minimum yield strength specified for the pipe that is being welded, a weld deposit yield strength of 79.8 ksi (550 MPa) minimum, 84.8 ksi (585 MPa) minimum, and 94.5 ksi minimum (652 MPa) is need for X-65, X-70, and X-80 pipe, respectively.
[0020] Table 1, shows the typical and expected maximum yield strengths of the X-65, X70, and X-80 pipe, the typical minimum yield strengths required for weld deposits in these pipes, the desired minimum weld strengths of the inventive weld deposit in these pipes, the yield strengths of weld deposits of seven commercially available welding filler metals, some of which have been used for X-65 and lower strength pipe, and the yield strengths for five weld deposits made according to the present invention. Table 2 shows the compositions for the welding filler metals listed in Table 1. All seven of the commercially available welding filler metals, including precipitation hardening alloy INCO-WELD® 725NDUR, suffer low, inconsistent, as-welded strength and none of the weld deposits made using the seven commercially available welding filler metals have sufficient yield strength to consistently meet the requirements of the higher strength pipe. Other precipitation-hardening, corrosion resistant welding wires are available, but they require time-consuming post weld heat treatment (pwht) to achieve sufficient strength which makes them unattractive.
- 5 2015240681 17 Oct 2017
Table 1 - Mechanical Properties of Pipes and Weld deposits
Alloy | Minimum Required Yield Strength (ksi)/(MPa) | Typical Yield Strength (ksi) /(MPa) | Expected Maximum Yield Strength (ksi) /(MPa) | Typical Weld Deposit Minimum Yield Strength (ksi) /(MPa) | Charpy VNotch Toughness (ft-lb.)/(J) | Desired Inventive Weld Deposit Minimum Yield Strength (ksi) /(MPa) |
Pipe | ||||||
X-65 | 65/448 | 72-74/ 496-510 | 75-77/ 517-531 | 78-82/ 538-565 Required | 79.8/550 | |
X-70 | 70/483 | 75-77/ 517-531 | 80-82/ 552-565 | 83-85/ 573-586 Required | 84.8/585 | |
X-80 | 80/552 | 84-86/ 579-593 | 88-90/ 607-621 | 90-93/ 621-641 Required | 94.5/652 | |
Prior Art Welding Fii | er Metals | |||||
INCO-WELD® C-276 | 60-70/ 414-483 | 30-50/ 41-68 | ||||
INCONEL® Alloy 625 | 65-75/ 448-517 | 25-45/ 34-61 | ||||
INCONEL® Alloy 622 | 65-75/ 448-517 | 30-45/ 41-61 | ||||
INCO-WELD® 686CPT® | 65-75/ 448-517 | 20-50/ 27-68 | ||||
Phy weld NOW | 65-75/ 448-517 | 20-50/ 27-68 | ||||
Alloy 59 | 65-75/ 448-517 | 20-50/ 27-68 | ||||
INCO-WELD® 725NDLR | 65-76/ 448-524 | 30-50/ 41-68 | ||||
230-W® | 68-78/ 469-538 | |||||
Inventive Welding Fi | ler Metals | |||||
HV1652 | 85.5/590 | |||||
HV1653 | 84.4/582 | |||||
HV1654 | 86.6/597 | |||||
HV1655 | 92.4/637 | |||||
HV1708 | >86.7/>598 | 137/186 |
-62015240681 17 Oct 2017
Table 2 - Nominal and Actual Chemical Compositions of the Welding
Filler Metals Shown in Table 1
Alloy | Ni | Cr | Fe | Nb | Ti | W | Mo | Al | C |
Nominal Compositions - Prior Art Welding Filler A | etals | ||||||||
INCO-WELD® C-276 | balance | 16 | 5 | 0.02 | 4 | 16 | 0.02 | ||
INCONEL® Alloy 625 | balance | 21 | 1 | 3.5 | 0.25 | 0.01 | 9 | 0.3 | 0.02 |
INCONEL® Alloy 622 | balance | 21 | 2 | 0.01 | 3 | 14 | 0.015 | ||
INCO-WELD® 686CPT® | balance | 21 | 1 | 0.01 | 0.25 | 4 | 16 | 0.5 | 0.01 |
Phy we Id NCW | balance | 22 | 2 | 0.2 | 0.4 | 3 | 10 | 0.4 | 0.03 |
Alloy 59 | balance | 23 | 1.5 | 16 | 0.3 | 0.01 | |||
INCO-WELD® 725NDUR | 57 | 21.5 | balance | 3.5 | 1.5 | 8.5 | 0.35 | 0.03 | |
230-W® | Balance | 22.0 | 3 | 14 | 2 | 0.35 | 0.10 | ||
Actual Compositions - Inventive Filler | Metals | ||||||||
HV1652 | 64.3 | 20.6 | <1.0 | 3.7 | 1.5 | 3.2 | 6.2 | 0.30 | 0.01 |
HV1653 | 62.2 | 20.7 | <1.0 | 3.6 | 1.5 | 3.3 | 8.3 | 0.31 | 0.01 |
HV1654 | 61.7 | 20.5 | <1.0 | 3.8 | 1.6 | 5.8 | 6.2 | 0.29 | 0.01 |
HV1655 | 58.8 | 20.4 | <1.0 | 3.8 | 1.5 | 6.9 | 6.9 | 0.27 | 0.01 |
HV1708 | 58.8 | 20.2 | <1.0 | 3.7 | 1.5 | 7.9 | 7.2 | 0.20 | 0.01 |
[0021] The present invention is directed to a welding filler metal comprising: 17.0 to 23.0% chromium, 5.0 to 12.0% molybdenum, 3.0 to 11.0% tungsten, 3.0 to 5.0% niobium, 0 to 2.0% tantalum, 1.2 to 3.0% titanium, 0.005 to 1.50% aluminum, 0.0005 to 0.100% carbon, less than 2.0% iron, less than 5.0% cobalt, and balance nickel wherein the nickel is 56.0 to 65.0%, preferably comprising 19.0 to 21.0% chromium, 6.0 to 9.0% molybdenum, 4.0 to 8.0% tungsten, 3.5 to 4.0% niobium, 0 to 1.0% tantalum, 1.4 to 2.0% titanium, 0.20 to 1.00% aluminum, 0.005 to 0.050% carbon, less than 0.5% iron, less than 2.5% cobalt, and balance nickel, wherein the nickel is 58.0 to 62.0%.
[0022] Nickel (Ni) - Nickel is beneficial for providing a ductile, corrosion resistant matrix capable of dissolving the above amounts of solute atoms. To achieve the desired effect, the nickel content is controlled to be at least 56.0%, preferably at least 57.0%, and more preferably 58.0%. However, excessive amounts of nickel have a detrimental effect on limiting the amount of strengthening and corrosion-resisting elements. Accordingly, the nickel content is controlled to be at most 65.0%, preferably at most 64.0%, and more preferably at most 62.0%.
- 7 2015240681 17 Oct 2017 [0023] Chromium (Cr) - Chromium is beneficial for corrosion resistance and some strengthening. To achieve the desired effect, the chromium content is controlled to be at least 17.0%, preferably at least 18.0%, and more preferably at least 19.0%. However, excessive amounts of chromium have a detrimental effect on CTE and ductility. Accordingly, the chromium content is controlled to be at most 23.0%, preferably at most 22.0%, and more preferably at most 21.0%.
[0024] Aluminum (Al) - Aluminum is beneficial for deoxidizing the filler metal and providing gamma prime strengthening. To achieve the desired effect, the aluminum content is controlled to be at least 0.005%, preferably at least 0.10%, more preferably at least 0.15%, and even more preferably at least 0.20%. However, excessive amounts of aluminum have a detrimental effect on hot-cracking resistance and surface cleanliness. Accordingly, the aluminum content is controlled to be at most 1.50%, preferably at most 1.25%, and more preferably at most 1.00%.
[0025] Niobium (Nb) - Niobium is beneficial for strengthening by precipitation of second phase particles. To achieve the desired second phases, the niobium content is controlled to be at least 3.0%, preferably at least 3.3%, and more preferably at least 3.5%. However, too much niobium can increase hot-cracking sensitivity. Accordingly, the niobium content is controlled to 5.0% maximum, preferably 4.5% maximum, and more preferably 4.0% maximum.
[0026] Molybdenum (Mo) - Molybdenum is beneficial for corrosion resistance and solid solution matrix strengthening. It also forms Mu phase which strengthens the welding filler metal. To achieve the desired effect, the molybdenum content is controlled to be at least 5.0%, preferably at least 5.5%, and more preferably at least 6.0%. However, higher amounts of molybdenum can complicate hot working of the welding filler metal during production. Accordingly, the molybdenum content is controlled to at most 12.0%, preferably at most 10.5%, and more preferably at most 9.0%.
[0027] Tungsten (W) - Tungsten is beneficial for strengthening and corrosion resistance. To achieve the desired effect, the tungsten content is controlled to be at least 3.0%, preferably at least 3.5%, and more preferably at least 4.0%, and at most 11.0%, preferably at most 9.5%, and more preferably at most 8.0%.
[0028] Tantalum (Ta) - Tantalum is beneficial for strengthening, like Nb, and may be adjusted in relationship to the Nb for control of microstructural phases. Under commercial conditions, tantalum would be expected to be present in an amount of at least 1 ppm even if
- 8 2015240681 17 Oct 2017 not intentionally added. Tantalum should not exceed 2.0%, preferably should not exceed
1.5%, and more preferably should not exceed 1.0%.
[0029] Niobium + Tantalum (Nb + Ta) - Niobium and tantalum are both second phase formers and strengtheners and, thus, may be adjusted for control of second phases; however, the total is at least 3.0%, preferably at least 3.3%, and more preferably at least 3.5% and at most 7.0%, preferably at most 6.0%, and preferably at most 5.0%.
[0030] Titanium (Ti) - Titanium is beneficial for porosity control and gamma prime formation as well as second phase formation. To achieve the desired effect, the titanium content is controlled to be at least 1.2%, preferably at least 1.3%, and more preferably at least 1.4%. However, too much titanium causes the formation of eta phase. Accordingly, the titanium content is controlled to at most 3.0%, preferably at most 2.5%, and more preferably at most 2.0%.
[0031] Carbon (C) - Carbon in conjunction with Ti and Nb is beneficial for grain size control of the as-welded weld deposit as well as second phase formation. To achieve the desired effect, the carbon content is controlled to be at least 0.0005%, preferably at least 0.005%, and more preferably at least 0.010% and at most 0.100%, preferably at most 0.075, and more preferably at most 0.050%.
[0032] Cobalt (Co) - Cobalt is a matrix-strengthening element that contributes in a measurable way to increase hardness and higher tensile and yield strengths. However, because of cost, it is desirable to limit its addition to 5.0% maximum, preferably to 4.0% maximum and, more preferably to 2.5% maximum.
[0033] Iron (Fe) - Iron in the welding tiller metal should be controlled to less than 2.0%, preferably to less than 1.0%, and more preferably to less than 0.5% in order to assist in maintaining low iron in the weld deposit. Excessive iron in the weld deposit decreases the yield strength in the as-welded condition.
]0034] Silicon (Si) - Silicon is helpful for improving puddle fluidity in small amounts, but can lead to increased sensitivity to hot-cracking or solidification cracking at higher levels. Accordingly, the silicon content is controlled to at most 0.75%, preferably 0.50% or less, more preferably 0.25% or less, and most preferably 0.15% or less.
[0035] Manganese (Mn) - Manganese should be at most 3.0%, preferably 2.0% or less, more preferably 1.0% or less, and most preferably 0.20% or less to discourage M23C6 formation.
[0036] Sulfur (S), Phosphorous (PE Calcium (Ca), and Magnesium (Mg) - Sulfur and phosphorous may be present as impurities and should be limited as follows: sulfur less than -92015240681 17 Oct 2017
0.002%, phosphorous less than 0.010%, and more preferably less than 0.005%, while calcium and magnesium may be added and should be controlled to calcium less than 0.006%, and more preferably less than 0.005%, and magnesium less than 0.020%, and more preferably less than 0.010%.
[0037] Five welding filler metals having the inventive composition were produced. The compositions of these welding filler metals are show in Table 2. Duplicate mechanical property testing was performed on four of the inventive welding deposits in the as-welded condition using longitudinal all-weld-metal specimens made using gas tungsten arc welding (GTAW). Two conditions were tested. The first having 15-20% iron dilution of the welding filler metal and the second having less than 5% iron dilution of the welding filler metal. The results are shown in Tables 3 and 4, a comparison of which shows that high iron dilution has a detrimental effect on yield strength.
[0038] Table 5 a shows Charpy V notch impact properties of a fifth inventive welding filler metal in the as-welded condition with less than 5% iron dilution and can be compared to the values given in Table 5b when the weld contains 9.4% Fe.
Table 3 - Mechanical Properties of As-Welded Longitudinal
All-Weld-Metal Specimens Having 15-20% Iron Dilution
0.2% Yield Strength | Ultimate Tensile Strength | Elongation (%) | Reduction of Area (%) | |||
ksi | MPa | ksi | MPa | |||
HV1652 | 65.3 | 450 | 111.7 | 770 | 27.6 | 30.1 |
64.7 | 446 | 109.7 | 756 | 27.9 | 36.7 | |
HV1653 | 67.3 | 464 | 112.7 | 777 | 42.1 | 46.3 |
65.4 | 451 | 108.2 | 746 | 25.6 | 31.0 | |
HV1654 | 70.9 | 489 | 114.4 | 789 | 28.3 | 32.9 |
68.4 | 472 | 115.7 | 798 | 32.9 | 31.8 | |
HV1655 | 70.7 | 488 | 115.3 | 795 | 25.5 | 29.2 |
70.0 | 483 | 119.3 | 823 | 32.6 | 36.7 |
Table 4 - Mechanical Properties of As-Welded Longitudinal
All-Weld-Metal Specimens Having Less Than 5% Iron Dilution
0.2% Yield Strength | Ultimate Tensile Strength | Elongation (%) | |||
ksi | MPa | ksi | MPa | ||
HV1652 | 85.6 | 590 | 129 | 889 | 45.4 |
85.4 | 589 | 128 | 883 | 41.1 |
- 102015240681 17 Oct 2017
HV1653 | 85.9 | 592 | 125 | 862 | 33.4 |
82.9 | 572 | 127 | 876 | 41.0 | |
HV1654 | 87.7 | 605 | 130 | 896 | 43.0 |
85.5 | 590 | 129 | 889 | 43.2 | |
HV1655 | 92.9 | 641 | 134 | 924 | 33.0 |
91.8 | 633 | 129 | 889 | 31.3 |
Table 5a - -50°F Weld Center Impact Values for Inventive Welding Filler Metal
HV1708
GTA Welc | ed to INCONEF1' 600 Base Material with Weld De | oosit Fe = 1.5%Fe* | ||||
Test# | Ft.-Lb. | Joules | 2 Joules/cm | Lat. Exp | %Shear | Broke (Y/N) |
1 | 152.8 | 207.2 | 259.0 | 0.094 | 85 | Y |
2 | 134.1 | 181.8 | 227.3 | 0.089 | 85 | Y |
3 | 124.2 | 168.4 | 210.5 | 0.078 | 85 | Y |
Average | 137.0 | 185.8 | 232.3 |
* determination made using Niton XL3T - Xrav Fluorescence Analyzer
Table 5b - -50°F Weld Center Impact Values for Inventive Welding Filler Metal HV1708 GTA Welded to INCONEF® alloy 625 I.D. Clad X-65 Steel Pipe with Weld Deposit Fe = 9.4%Fe
Test# | Ft.-Lb. | Joules | Joules/cm | Lat. Exp | %Shear |
1 | 46.6 | 63.2 | 79.0 | 0.022 | 20 |
2 | 36.9 | 50.0 | 62.5 | 0.021 | 20 |
3 | 44.8 | 60.7 | 75.9 | 0.029 | 20 |
Average | 42.8 | 58.0 | 72.5 |
[0039] As can be seen from the mechanical properties in Tables 3, 4, 5a, and 5b, when the inventive welding filler metals are diluted with 15%-20% Fe, the yield strength is about 20 ksi (138 MPa) lower than when the iron dilution is less than 5%. Also, when the inventive welding filler metals are diluted with more than 9% Fe, the impact properties are considerably lower than when dilution is controlled to less than 5% Fe. Thus, the Fe in the weld deposit should be kept below 8.0%, preferably below 7.0%, and more preferably below 5.0%. Iron dilution can be controlled to low values by maintaining low heat input which in turn maintains second phase particle fineness while promoting higher yield and impact strengths. For highest values of yield and impact strengths, the heat input of welding should be less than 50 kJ/in., preferably less than 45 kJ/in., and more preferably less than 40 kJ/in. At the same time, lower heat input usually calls for more weld beads or passes which in turn increases the strengthening of previous beads or passes with the heat input of subsequent beads or passes.
- 11 2015240681 17 Oct 2017 [0040] The weld deposit has a yield strength of at least 72 ksi (496 MPa), preferably at least 78 ksi (538 MPa), and more preferably at least 80 ksi (552 MPa), elongation of at least 20%, preferably at least 25%, and more preferably at least 30%, toughness of at least 50 J at 50°F, preferably at least 70 J at -50°F, and more preferably at least 100 J at -50°F, and hardness between 200-400 HV.
[0041] The microstructure of the weld deposit contains second phase particles in the interdendritic areas. The second phase particles are shown in FIG. 1 which is a scanning electron micrograph of the microstructure of a weld deposit made using inventive welding filler metal HV 1655. The second phase particles are principally less than 5 μιη and may be less than 0.5 μιη.
[0042] The second phase particles are precipitated upon solidification and cool-down into a matrix that is stiffened with tungsten and molybdenum, and this combination, coupled with the strengthening effect of multiple weld beads or passes, provides the unexpectedly high yield strength. The fineness and density of the particles contribute to the extremely high impact toughness and high elongation of the weld deposit. Such a combination is unexpected in a very high strength nickel alloy weld deposit since as strength is increased in prior art weld deposits, toughness and ductility are generally decreased.
[0043] As can be seen for the prior art welding filler metals that do not contain substantial amounts of niobium and titanium (INCO-WELD® C-276, INCONEL® Alloy 622, INCOWELD® 686CPT®, Phyweld NOW, Alloy 59), yield strengths of the weld deposit in the 6065 ksi (414-448 MPa) range are attained. Also, tensile testing of 230-W® filler metal weld deposits determined the yield strength to be in the 68-78 ksi (469-538 MPa) range. Thus, high tungsten of 14% along with 3% molybdenum in a nickel matrix without niobium and titanium additions does not produce the high weld deposit yield strengths of the inventive welding filler metal. The 3.0-5.0% niobium and 1.2-3.0% titanium in the inventive welding filler metal coupled with low iron in the welding filler metal and low iron dilution from the welding process produce yield strengths on the order of 72-92 ksi (496-634 MPa). Also, when heat input of the welding process is controlled to lower values with low iron in the filler metal and low iron dilution in the weld, it is believed that yield strengths on the order of 8395 ksi (572-655 MPa) can be produced.
[0044] Prior art welding filler metals have focused on the control of second phases by heat treatment; however, since the precipitation and control devices for the inventive welding filler metal are in effect from melting through solidification and cool-down, the inventive
- 122015240681 17 Oct 2017 filler metal can be used in the as-welded condition to achieve high speed fabrication along with high weld deposit strength.
[0045] Commercially available certified 4” diameter INCONEL* alloy 625 ID clad X-65 pipe was obtained for testing of the inventive welding filler metal. Mechanical testing of unwelded samples of the pipe determine the yield strength to be 87.2 ksi (601 MPa) (average of four tests, Table 6). Based on the mechanical properties, this lot of pipe could have been double or triple qualified as X-65, X-70, and X-80 pipe. Table 7 gives the composition of this lot of pipe. Since this pipe could have been double or triple qualified as X-65, X-70, or X-80 pipe, the typical compositions of X-70 and X-80 pipe would be similar with slightly higher Mn, around 1.5-1.7%.
Table 6 - Mechanical Properties of Unwelded X-65 Pipe
Sample I.D. | 0.2% Yield Strength | Ultimate Tensile Strength | Elongation (%) | Reduction of Area (%) | Hardness (HRB) | ||
ksi | MPa | ksi | MPa | ||||
1 | 87.7 | 605 | 101.7 | 701 | 27.0 | 77.0 | 95.8 |
2 | 87.2 | 601 | 100.9 | 696 | 28.3 | 77.2 | 95.5 |
3 | 86.5 | 596 | 100.8 | 695 | 25.8 | 77.6 | 95.3 |
4 | 87.4 | 603 | 101.5 | 700 | 25.1 | 76.8 | 96.1 |
Average | 87.2 | 601 | 101.2 | 698 | 26.6 | 77.2 | 95.7 |
Table 7 -Composition of X-65 Pipe Used to Make the Experimental Welds
Fe | C | Mn | Si | Cr | Mo | Cu | Al | Nb | V |
balance | 0.11 | 1.25 | 0.31 | 0.10 | 0.20 | 0.14 | 0.04 | 0.04 | 0.05 |
[0046] Circumferential groove welds were produced in the X-65 pipe using inventive welding filler metals HV1654, HV1655, and HV1708 using the GTAW process with low Fe dilution techniques in which only enough of the sidewalls were melted to obtain fusion with very little penetration into the sidewalls. Transverse tensile tests were performed on the welded pipes. Both T-2 and T-3 specimens were prepared and tested. Table 8 shows the transverse tensile results for the welded pipes made with the HV1654 welding filler metal and shows that all of the specimens failed in the base metal away from the heat affected zone (HAZ) and fusion line. FIG. 2 shows two of the specimens after tensile testing. These results indicate that the strength of the welding filler metal HV1654 is greater than 80.9 ksi (558 MPa) when used to weld X-65 pipe. Transverse bend tests were also performed and passed without flaws.
- 13 2015240681 17 Oct 2017 [0047] Table 9 shows the results of transverse tensile tests for the X-65 pipe welded using welding filler metal HV1708. All of the specimens failed in the base metal away from the fusion line and the HAZ. These results indicate that the strength of welding filler metal HV1708 is greater than 86.7 ksi (598 MPa) when used to weld X-65 pipe. FIG. 3 shows the failed tensile specimens.
Table 8 - Transverse Tensile Properties for INCONEL* Alloy 625 I.D. Clad X-65 pipe
GTAW Welded with Inventive Welding Filler Metal HV1654
Sample I.D. | Sample | 0.2% Yield Strength | Ultimate Tensile Strength | Elongation (%) | Reduction of Area (%) | Failure Location | ||
ksi | MPa | ksi | MPa | |||||
Continuous orbital pipe welc | made using a | positioner | ||||||
1 | T3 | 72.3 | 499 | 91.5 | 631 | 23.6 | 75.4 | Base Material |
2 | T3 | 72.6 | 501 | 91.9 | 634 | 24.8 | 72.6 | Base Material |
3 | T2 | 78.7 | 543 | 95.3 | 657 | 22.2 | 76.0 | Base Material |
4 | 12 | 76.6 | 528 | 94.1 | 649 | 25.2 | 76.8 | Base Material |
Manual | pipe weld made one quadrant at a time then rotatec | |||||||
1 | T3 | 74.1 | 511 | 92.2 | 636 | 23.2 | 75.0 | Base Material |
2 | T3 | 73.9 | 510 | 92.8 | 640 | 23.8 | 75.4 | Base Material |
3 | T2 | 80.9 | 558 | 98.1 | 676 | 21.6 | 74.4 | Base Material |
4 | T2 | 77.6 | 535 | 94.8 | 654 | 19.9 | 75.1 | Base Material |
Table 9 - Transverse Tensile Properties for INCONEL^ Alloy 625 I.D. Clad X-65 pipe
GTAW Welded with Inventive Welding Filler Metal HV1708
Sample I.D. | 0.2% Yield Strength | Ultimate Tensile Strength | Elongation (%) | Reduction of Area (%) | Failure Location | ||
ksi | MPa | ksi | MPa | ||||
1 | 81.5 | 562 | 98.4 | 678 | 23.2 | 77.7 | Base Material |
2 | 86.7 | 598 | 100.1 | 690 | 23.3 | 76.8 | Base Material |
3 | 82.7 | 570 | 101.4 | 699 | 21.2 | 72.1 | Base Material |
4 | 82.2 | 567 | 99.9 | 689 | 21.5 | 76.6 | Base Material |
[0048] Based on the foregoing data, it can be seen that the inventive welding filler metal can be used for joining high strength INCONEL^ alloy 625 ID clad X-65, X-70, and X-80 steel pipe and produces acceptable bend tests and tensile tests that fail in the base metal. These weld deposits are stronger than the base metal in the as-welded condition and provide very high toughness in Charpy V notch testing at -50°F. It is unexpected that both high yield strength and toughness are present in the as-welded condition. This combination of properties is produced by a fine dispersion of second phase particles within a matrix of
- 142015240681 17 Oct 2017 molybdenum and tungsten stiffened nickel and chromium. These particles are precipitated from the melt during solidification and cool-down and provide as-welded properties that have not been achieved with any prior art corrosion-resistant nickel based welding filler metals. Based on the Cr, Mo, and W in the nickel matrix, these weld deposits should exhibit good corrosion resistance that is at least equal to that of INCONEL® alloy 625 weld deposits when tested in ASTM G-48 environments. Crack tip opening displacement (CTOD) results and fatigue resistance should also be good.
[0049] The welding filler metal may be supplied in any suitable form including tubular wire and flux cored wire. The solid wires are produced as conventional solid solution nickel alloys, but require relatively high temperature annealing and must be annealed more frequently than other nickel alloys. The process includes conventional vacuum melting, casting of an ingot, which may be remelted, and hot working the ingot to form billets. The billets are then hot-rolled to form wire/rod. The wire/rod is cold drawn to a tensile strength of over 200 ksi (1379 MPa), annealed above 2000°F (1093°C), and redrawn to finished sizes. In the annealed condition, the wires may have a tensile strength of 120-140 ksi (827-965 MPa).
[0050] The welding filler metal may be used with any suitable welding process, preferably gas metal arc welding (GMAW) or gas tungsten arc welding (GTAW). During the welding process, the welding filler metal will be melted and cooled to form a weld deposit. To reduce welding time and iron dilution of the weld deposit, it is preferred that the included angle of the weld joint be small, 2-5 degrees, often called a narrow groove, and that a vertical down GMAW welding process be used to reduce the heat input and allow for relatively fast travel of the welding process. In addition, if INCONEL® alloy 625 or similar alloy ID clad high strength steels are being welded, the cladding will provide a base (root of the joint already fused) of 3-4 mm of INCONEL® alloy 625 or similar weld metal that will limit the amount of iron dilution to only that coming from the sidewalls of the joint.
[0051] The welding filler metal and method described above may be used to produce a weldment comprising at least two high-strength steel components joined by a weld deposit made using the inventive welding filler metal and having the properties described above. Also, as mentioned above the at least two high-strength steel components may be selected from X-65, X-70, or X-80 pipes that may have ID cladding of INCONEL® alloy 625.
[0052] Although the invention has been described in detail for the purpose of illustration based on what is currently considered to be the most practical and preferred embodiments, it is to be understood that such detail is solely for that purpose and that the invention is not
- 15 2015240681 17 Oct 2017 limited to the disclosed embodiments but, on the contrary, is intended to cover modifications and equivalent arrangements that are within the spirit and scope of the appended claims. For example, it is to be understood that the present invention contemplates that, to the extent possible, one or more features of any embodiment can be combined with one or more features of any other embodiment.
- 162015240681 17 Oct 2017
Claims (19)
- THE INVENTION CLAIMED ISE A welding filler metal comprising, in weight percent: 17.0 to 23.0% chromium, 5.0 to 12.0% molybdenum, 3.0 to 11.0% tungsten, 3.0 to 5.0% niobium, 0 to 2.0% tantalum, 1.2 to 3.0% titanium, 0.005 to 1.50% aluminum, 0.0005 to 0.100% carbon, less than 2.0% iron, less than 5.0% cobalt, and balance nickel wherein the nickel is 56.0 to 65.0%, and wherein a weld deposit formed from the welding tiller metal has a minimum yield strength in an as-welded condition of at least 72 ksi (496 MPa).
- 2. The welding filler metal of claim 1 comprising a minimum of 3.5% niobium + tantalum.
- 3. The welding filler metal of claim 1 comprising a maximum of 6.0% niobium + tantalum.
- 4. A welding filler metal product comprising, in weight percent: 17.0 to 23.0% chromium, 5.0 to 12.0% molybdenum, 3.0 to 11.0% tungsten, 3.0 to 5.0% niobium, 0 to 2.0% tantalum, 1.2 to 3.0% titanium, 0.005 to 1.50% aluminum, 0.0005 to 0.100% carbon, less than 2.0% iron, less than 5.0% cobalt, and balance nickel wherein the nickel is 56.0 to 65.0%, and wherein a weld deposit formed from the welding filler metal product has a minimum yield strength in an as-welded condition of at least 72 ksi (496 MPa).
- 5. The welding filler metal product of claim 4 comprising a minimum of 3.5% niobium + tantalum.
- 6. The welding filler metal product of claim 4 or 5 comprising a maximum of 6.0% niobium + tantalum.
- 7. The welding filler metal product of claim 4, 5 of 6, wherein the product is in the form of a tubular wire or a flux-cored wire.- 172015240681 17 Oct 2017
- 8. A weld deposit comprising, in weight percent: 17.0 to 23.0% chromium, 5.0 to 12.0% molybdenum, 3.0 to 11.0% tungsten, 3.0 to 5.0% niobium, 0 to 2.0% tantalum, 1.2 to 3.0% titanium, 0.005 to 1.50% aluminum, 0.0005 to 0.100% carbon, less than 8.0% iron, less than 5.0% cobalt, and balance nickel wherein the nickel is 56.0 to 65.0%, and wherein the weld deposit has a minimum yield strength in an as-welded condition of at least 72 ksi (496 MPa).
- 9. The weld deposit of claim 8 comprising a minimum of 3.5% niobium + tantalum.
- 10. The weld deposit of claim 8 or 9 comprising a maximum of 6.0% niobium + tantalum.
- 11. The weld deposit of claim 8, 9 or 10 comprising a microstructure including finely dispersed second phase particles.
- 12. The weld deposit of claims 11, wherein the second phase particles are less than 5 pm.
- 13. The weld deposit of any one of claims 8 to 12, wherein elongation of the weld deposit is at least 20%.
- 14. The weld deposit of any one of claims 8 to 13, wherein toughness of the weld deposit is at least 50 J at -50°F.
- 15. A method of producing a weld deposit comprising:providing a welding filler metal comprising, in weight percent, 56.0 to 65.0% nickel, 17.0 to 23.0% chromium, 5.0 to 12.0% molybdenum, 3.0 to 11.0% tungsten, 3.0 to 5.0% niobium, 0 to 2.0% tantalum, 1.2 to 3.0% titanium, 0.005 to 1.50% aluminum, 0.0005 to 0.100% carbon, less than 2.0% iron, and less than 5.0% cobalt;melting and cooling the welding filler metal to create a weld deposit; and limiting iron dilution of the weld deposit during melting and cooling such that an as-welded weld deposit contains less than 8% iron,- 182015240681 17 Oct 2017 wherein the weld deposit has a minimum yield strength in the as-welded condition of at least 72 ksi (496 MPa).
- 16. The method of claim 15, wherein the melting and cooling of the welding filler metal is accomplished by gas metal arc welding (GMAW).
- 17. The method of claim 16, wherein the welding filler metal is melted and cooled in a narrow groove joint between two steel components wherein the narrow groove joint has an included angle of 2-5 degrees.
- 18. The method of claim 16, wherein the welding filler metal is melted and cooled in a narrow groove joint between two steel components wherein the steel components are clad on at least one side with a nickel alloy.
- 19. A weldment comprising:at least two high-strength steel components, each of the components individually having a minimum yield strength of 65 ksi (448 MPa) connected by a weld deposit comprising, in weight percent, 56.0 to 65.0% nickel, 17.0 to 23.0% chromium, 5.0 to 12.0% molybdenum, 3.0 to 11.0% tungsten, 3.0 to 5.0% niobium, 0 to 2.0% tantalum, 1.2 to 3.0% titanium, 0.005 to 1.50% aluminum, 0.0005 to 0.100% carbon, less than 8.0% iron, and less than 5.0% cobalt and having a minimum yield strength in an as-welded condition of at least 72 ksi (496 MPa).
Applications Claiming Priority (5)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US201461975358P | 2014-04-04 | 2014-04-04 | |
US61/975,358 | 2014-04-04 | ||
US201461989188P | 2014-05-06 | 2014-05-06 | |
US61/989,188 | 2014-05-06 | ||
PCT/US2015/024138 WO2015153905A1 (en) | 2014-04-04 | 2015-04-02 | High strength ni-cr-mo-w-nb-ti welding product and method of welding and weld deposit using the same |
Publications (2)
Publication Number | Publication Date |
---|---|
AU2015240681A1 AU2015240681A1 (en) | 2015-10-08 |
AU2015240681B2 true AU2015240681B2 (en) | 2018-05-10 |
Family
ID=54241295
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
AU2015240681A Active AU2015240681B2 (en) | 2014-04-04 | 2015-04-02 | High strength Ni-Cr-Mo-W-Nb-Ti welding product and method of welding and weld deposit using the same |
Country Status (9)
Country | Link |
---|---|
US (1) | US9815147B2 (en) |
EP (2) | EP3431222B1 (en) |
JP (1) | JP6396574B2 (en) |
KR (2) | KR102025551B1 (en) |
CN (1) | CN106457481B (en) |
AU (1) | AU2015240681B2 (en) |
BR (1) | BR112016023139B1 (en) |
CA (1) | CA2944880C (en) |
WO (1) | WO2015153905A1 (en) |
Families Citing this family (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US9815147B2 (en) * | 2014-04-04 | 2017-11-14 | Special Metals Corporation | High strength Ni—Cr—Mo—W—Nb—Ti welding product and method of welding and weld deposit using the same |
DE102017129218A1 (en) * | 2017-12-08 | 2019-06-13 | Vdm Metals International Gmbh | WELDING MATERIAL |
CN109693055A (en) * | 2019-01-31 | 2019-04-30 | 江苏新航合金科技有限公司 | Oil-gas pipeline inner wall overlaying corrosion-and high-temp-resistant nickel alloy welding wire and preparation method |
CN110605501B (en) * | 2019-09-18 | 2021-09-03 | 中国电建集团上海能源装备有限公司 | Low-toxicity nickel-based welding rod for welding Ni-Cr-Mo alloy steel and preparation thereof |
CN111318835B (en) * | 2020-04-03 | 2022-03-15 | 中国科学院金属研究所 | Nickel-based alloy welding wire for high-temperature alloy fusion welding and preparation method and application thereof |
CN112192001B (en) * | 2020-08-18 | 2022-05-06 | 江阴兴澄特种钢铁有限公司 | Submerged-arc welding method for marine 5Ni steel |
CN113732561A (en) * | 2021-08-19 | 2021-12-03 | 江苏新航合金科技有限公司 | Nickel-based high-temperature alloy welding material for aviation |
CN114535858B (en) * | 2022-01-11 | 2023-12-29 | 郑州天时海洋石油装备有限公司 | Welding material for preparing high-strength copper-steel gradient structure by CMT and preparation method |
CN116117381B (en) * | 2023-04-12 | 2023-08-18 | 西安热工研究院有限公司 | Double-precipitation reinforced Ni-Cr welding wire, manufacturing method thereof and welding process |
CN116275706B (en) * | 2023-05-24 | 2023-08-11 | 北京煜鼎增材制造研究院股份有限公司 | High-energy beam fuse deposition additive preparation method of nickel-based superalloy |
Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5725693A (en) * | 1996-03-06 | 1998-03-10 | Lockheed Martin Energy Systems, Inc. | Filler metal alloy for welding cast nickel aluminide alloys |
US20040136301A1 (en) * | 2002-07-25 | 2004-07-15 | Tsung-Huei Ren | Optical recording system with a built-in jitter |
US20120118936A1 (en) * | 2010-11-12 | 2012-05-17 | Kabushiki Kaisha Kobe Seiko Sho (Kobe Steel, Ltd.) | Ni BASE ALLOY SOLID WIRE FOR WELDING |
Family Cites Families (52)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2400255A (en) * | 1941-05-27 | 1946-05-14 | Int Nickel Co | Electric resistance elements and the like |
DE1208595B (en) | 1961-05-06 | 1966-01-05 | Deutsche Edelstahlwerke Ag | Process for the creation of chrome diffusion zones with extremely low surface roughness on parts made of nickel or cobalt alloys |
BE635019A (en) * | 1962-11-21 | |||
US3311972A (en) * | 1964-08-17 | 1967-04-04 | Int Nickel Co | Production of ingots for wrought metal products |
GB1070099A (en) * | 1965-06-25 | 1967-05-24 | Int Nickel Ltd | Welding high-temperature alloys |
US3512963A (en) * | 1966-07-25 | 1970-05-19 | Int Nickel Co | Process for improving elevated temperature strength and ductility of nickel-base alloys |
US3632319A (en) * | 1969-07-11 | 1972-01-04 | Gen Electric | Diffusion bonding of superalloy members |
JPS5631345B2 (en) * | 1972-01-27 | 1981-07-21 | ||
US3785877A (en) * | 1972-09-25 | 1974-01-15 | Special Metals Corp | Treating nickel base alloys |
US3865575A (en) * | 1972-12-18 | 1975-02-11 | Int Nickel Co | Thermoplastic prealloyed powder |
SU780374A1 (en) * | 1979-06-20 | 1990-04-07 | Предприятие П/Я А-3700 | Welding eleclode wire composition |
US4359352A (en) * | 1979-11-19 | 1982-11-16 | Marko Materials, Inc. | Nickel base superalloys which contain boron and have been processed by a rapid solidification process |
DE3030532A1 (en) * | 1980-08-13 | 1982-03-18 | Brown, Boveri & Cie Ag, 6800 Mannheim | METHOD FOR RIP-FREE ENERGY BEAM WELDING OF HEAT-RESISTANT MOLDED PARTS |
US5556594A (en) * | 1986-05-30 | 1996-09-17 | Crs Holdings, Inc. | Corrosion resistant age hardenable nickel-base alloy |
IL82587A0 (en) | 1986-05-27 | 1987-11-30 | Carpenter Technology Corp | Nickel-base alloy and method for preparation thereof |
US4765956A (en) * | 1986-08-18 | 1988-08-23 | Inco Alloys International, Inc. | Nickel-chromium alloy of improved fatigue strength |
US5328499A (en) * | 1993-04-28 | 1994-07-12 | Inco Alloys International, Inc. | Mechanically alloyed nickel-base composition having improved hot formability characteristics |
JPH07227693A (en) * | 1994-02-17 | 1995-08-29 | Nippon Steel Corp | Welding wire for cryogenic steel |
WO1997038144A1 (en) * | 1996-04-10 | 1997-10-16 | The Penn State Research Foundation | Improved superalloys with improved oxidation resistance and weldability |
DK173348B1 (en) * | 1996-06-07 | 2000-08-07 | Man B & W Diesel As | Exhaust valve for an internal combustion engine |
JP3542702B2 (en) * | 1997-07-30 | 2004-07-14 | 株式会社エヌゼットケイ | Valve stem for diesel engine |
WO2000003053A1 (en) * | 1998-07-09 | 2000-01-20 | Inco Alloys International, Inc. | Heat treatment for nickel-base alloys |
EP1154027B1 (en) * | 1999-01-28 | 2004-11-10 | Sumitomo Electric Industries, Ltd. | Heat-resistant alloy wire |
US6242113B1 (en) * | 1999-06-10 | 2001-06-05 | Inco Alloys International, Inc. | Welding alloy and articles for use in welding, weldments and methods for producing weldments |
US6544668B1 (en) * | 1999-09-15 | 2003-04-08 | U. T. Battelle, Llc | Ductile filler metal alloys for welding nickel aluminide alloys |
US6302649B1 (en) * | 1999-10-04 | 2001-10-16 | General Electric Company | Superalloy weld composition and repaired turbine engine component |
US6354799B1 (en) * | 1999-10-04 | 2002-03-12 | General Electric Company | Superalloy weld composition and repaired turbine engine component |
JP2001107196A (en) * | 1999-10-07 | 2001-04-17 | Sumitomo Metal Ind Ltd | Austenitic steel welded joint excellent in weld cracking resistance and sulfuric acid corrosion resistance and the welding material |
DE19957646A1 (en) | 1999-11-30 | 2001-05-31 | Krupp Vdm Gmbh | Alloy production comprises coating base material made of austenitic nickel-based alloy or cobalt-based alloy or special steel on one or both sides with layer of aluminum or aluminum alloy |
CA2396578C (en) * | 2000-11-16 | 2005-07-12 | Sumitomo Metal Industries, Ltd. | Ni-base heat-resistant alloy and weld joint thereof |
US6489584B1 (en) * | 2001-05-08 | 2002-12-03 | General Electric Company | Room-temperature surface weld repair of nickel-base superalloys having a nil-ductility range |
JP4895434B2 (en) * | 2001-06-04 | 2012-03-14 | 清仁 石田 | Free-cutting Ni-base heat-resistant alloy |
JP3842717B2 (en) * | 2002-10-16 | 2006-11-08 | 株式会社日立製作所 | Welding material, welded structure, gas turbine rotor blade, and gas turbine rotor blade or stationary blade repair method |
US20040079453A1 (en) * | 2002-10-25 | 2004-04-29 | Groh Jon Raymond | Nickel-base alloy and its use in casting and welding operations |
KR100663720B1 (en) * | 2003-06-10 | 2007-01-02 | 수미도모 메탈 인더스트리즈, 리미티드 | Austenitic steel weld joint |
EP1841893B1 (en) * | 2005-01-25 | 2012-05-16 | Huntington Alloys Corporation | Coated welding electrode having resistance to ductility dip cracking, and weld deposit produced therefrom |
US20070095441A1 (en) * | 2005-11-01 | 2007-05-03 | General Electric Company | Nickel-base alloy, articles formed therefrom, and process therefor |
JP5201708B2 (en) * | 2006-04-14 | 2013-06-05 | 三菱マテリアル株式会社 | Ni-based heat-resistant alloy welding wire |
KR101399795B1 (en) * | 2006-08-08 | 2014-05-27 | 헌팅턴 앨로이즈 코오포레이션 | Welding alloy and articles for using in welding, weldments and method for producing weldments |
ES2444784T3 (en) * | 2006-10-02 | 2014-02-26 | Nippon Steel & Sumitomo Metal Corporation | Joint welded by electron beam with excellent fragile fracture resistance |
EP1914327A1 (en) * | 2006-10-17 | 2008-04-23 | Siemens Aktiengesellschaft | Nickel-base superalloy |
FR2910912B1 (en) * | 2006-12-29 | 2009-02-13 | Areva Np Sas | METHOD FOR THE HEAT TREATMENT OF ENVIRONMENTALLY ASSISTED CRACKING DISENSIBILIZATION OF A NICKEL-BASED ALLOY AND PART PRODUCED THEREBY THUS PROCESSED |
ES2534346T3 (en) * | 2007-11-19 | 2015-04-21 | Huntington Alloys Corporation | Ultra-high strength alloy for severe oil and gas environments and preparation method |
US20090321405A1 (en) * | 2008-06-26 | 2009-12-31 | Huntington Alloys Corporation | Ni-Co-Cr High Strength and Corrosion Resistant Welding Product and Method of Preparation |
JP5254693B2 (en) * | 2008-07-30 | 2013-08-07 | 三菱重工業株式会社 | Welding material for Ni-base alloy |
JP5566758B2 (en) * | 2009-09-17 | 2014-08-06 | 株式会社東芝 | Ni-based alloy for forging or rolling and components for steam turbine using the same |
US8618434B2 (en) * | 2010-03-22 | 2013-12-31 | Siemens Energy, Inc. | Superalloy repair welding using multiple alloy powders |
EP2455504A1 (en) * | 2010-11-19 | 2012-05-23 | Schmidt + Clemens GmbH + Co. KG | Nickel-chromium-iron-molybdenum alloy |
JP5389000B2 (en) * | 2010-12-02 | 2014-01-15 | 株式会社神戸製鋼所 | Ni-base alloy weld metal, Ni-base alloy-coated arc welding rod |
JP2013052441A (en) * | 2011-08-10 | 2013-03-21 | Hitachi Metals Ltd | Anvil for hot forging and hot forging method |
US20150217412A1 (en) * | 2014-01-31 | 2015-08-06 | General Electric Company | Weld filler for nickel-base superalloys |
US9815147B2 (en) * | 2014-04-04 | 2017-11-14 | Special Metals Corporation | High strength Ni—Cr—Mo—W—Nb—Ti welding product and method of welding and weld deposit using the same |
-
2015
- 2015-04-02 US US14/677,277 patent/US9815147B2/en active Active
- 2015-04-02 AU AU2015240681A patent/AU2015240681B2/en active Active
- 2015-04-02 BR BR112016023139-2A patent/BR112016023139B1/en active IP Right Grant
- 2015-04-02 KR KR1020187019290A patent/KR102025551B1/en active IP Right Grant
- 2015-04-02 WO PCT/US2015/024138 patent/WO2015153905A1/en active Application Filing
- 2015-04-02 CN CN201580029132.XA patent/CN106457481B/en active Active
- 2015-04-02 CA CA2944880A patent/CA2944880C/en active Active
- 2015-04-02 KR KR1020167030889A patent/KR101879221B1/en active IP Right Grant
- 2015-04-02 EP EP18180426.1A patent/EP3431222B1/en active Active
- 2015-04-02 JP JP2017503785A patent/JP6396574B2/en active Active
- 2015-04-02 EP EP15772300.8A patent/EP3126090B1/en active Active
Patent Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5725693A (en) * | 1996-03-06 | 1998-03-10 | Lockheed Martin Energy Systems, Inc. | Filler metal alloy for welding cast nickel aluminide alloys |
US20040136301A1 (en) * | 2002-07-25 | 2004-07-15 | Tsung-Huei Ren | Optical recording system with a built-in jitter |
US20120118936A1 (en) * | 2010-11-12 | 2012-05-17 | Kabushiki Kaisha Kobe Seiko Sho (Kobe Steel, Ltd.) | Ni BASE ALLOY SOLID WIRE FOR WELDING |
Also Published As
Publication number | Publication date |
---|---|
KR20180081177A (en) | 2018-07-13 |
JP2017515690A (en) | 2017-06-15 |
WO2015153905A1 (en) | 2015-10-08 |
US20150306710A1 (en) | 2015-10-29 |
EP3126090B1 (en) | 2018-08-22 |
EP3126090A1 (en) | 2017-02-08 |
KR102025551B1 (en) | 2019-09-26 |
EP3431222B1 (en) | 2020-01-22 |
EP3126090A4 (en) | 2017-09-20 |
KR20170021766A (en) | 2017-02-28 |
CN106457481B (en) | 2018-05-11 |
CN106457481A (en) | 2017-02-22 |
CA2944880C (en) | 2018-11-06 |
BR112016023139B1 (en) | 2021-05-18 |
KR101879221B1 (en) | 2018-07-17 |
JP6396574B2 (en) | 2018-09-26 |
EP3431222A1 (en) | 2019-01-23 |
CA2944880A1 (en) | 2015-10-08 |
US9815147B2 (en) | 2017-11-14 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
AU2015240681B2 (en) | High strength Ni-Cr-Mo-W-Nb-Ti welding product and method of welding and weld deposit using the same | |
JP4886440B2 (en) | High strength weld metal with excellent low temperature toughness | |
US8258432B2 (en) | Welding trip steels | |
CA2867673C (en) | Process for producing welded joint, and welded joint | |
KR20200079541A (en) | Gas shield arc welding wire and gas shield arc welding method | |
US20150034605A1 (en) | High fracture toughness welds in thick workpieces | |
Rizvi et al. | Effect of different welding parameters on the mechanical and microstructural properties of stainless steel 304h welded joints | |
US20220281038A1 (en) | Stainless steel welding wire for use in lng tank manufacturing | |
JP4745900B2 (en) | High strength weld metal with good low temperature toughness, low temperature cracking resistance and bead shape during all position welding | |
JPS63157795A (en) | Wire for high tensile steel | |
JP7502041B2 (en) | Welding materials for high Cr ferritic heat-resistant steel | |
KR102715916B1 (en) | Flux-cored wire, welded metal, gas-shielded arc welding method, and welded joint manufacturing method | |
JP2004261858A (en) | Wire for welding martensitic stainless steel pipe | |
JPH10180488A (en) | Flux cored wire for electro gas arc welding | |
Roy et al. | Studies on microstructure and mechanical properties of modified 9Cr–1Mo (P91) steel in submerged arc welding with TiO 2-enriched fluxes | |
RU2792989C1 (en) | Method for the production of longitudinally welded pipes of large diameter from low alloy steel | |
Gürol | Heat input effect of the FCAW process on the microstructure and mechanical properties of structural steel joints | |
Patel et al. | Experimental Study of the Effect of Heat Input on Mechanical Properties of TIG Welded Joints of SA516 Grade 70 Material | |
JPH09285891A (en) | Electro gas arc welding fluxed core wire | |
CN114850627A (en) | Flux-cored wire, weld metal, gas-shielded arc welding method, and method for manufacturing welded joint | |
Hou et al. | Weldability Evaluation of a New High Strength 9% Ni Steel for Cryogenic Applications | |
JP6483540B2 (en) | Gas shielded arc welding wire | |
Yamada et al. | Process for producing welded joint using GMA welding and CO 2 as a shielding gas | |
JP2021025096A (en) | Austenitic heat-resistant alloy weld joint |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
NB | Applications allowed - extensions of time section 223(2) |
Free format text: THE TIME IN WHICH TO ENTER THE NATIONAL PHASE HAS BEEN EXTENED TO 04 FEB 2017 |
|
FGA | Letters patent sealed or granted (standard patent) | ||
HB | Alteration of name in register |
Owner name: SPECIAL METALS LLC Free format text: FORMER NAME(S): SPECIAL METALS CORPORATION |